System Overview Flashcards

1
Q

What is the Aircrafts maximum takeoff weight

A

1950 pounds

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2
Q

How much approximate horsepower does each engine provide

A

56 hp

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3
Q

What is the engine displacement

A

800 cm³ or 0.8 L

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4
Q

How is the MQ –5B cooled

A

Liquid cooled 50/50 mix of water and glycol coolant

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5
Q

How is the power from the crankshaft transfer to the propellers

A

A centrical clutch transfers power from the crankshaft to the propeller through the propeller Drive assembly

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6
Q

What is the fuel capacity fuselage fuel tank

A

190+ or -5 L

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7
Q

What is the fuel capacity of the wing tanks

A

110+ or -5 L

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8
Q

Which electrical system components reduce 28 VDC to lower voltage required for other components

A

Converters

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9
Q

What the voltages do the converters outlet

A

15, -15, 12, & 5 VDC

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10
Q

Which component is the MQ – 5B Primary Attitude sensor

A

Primary sensor
INS Internal Navigation Sensor

Back up sensor
DMU Dynamic Measurement Unit

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11
Q

Which components is the MQ- 5B Primary altitude sensor

A

ADU Air Data Unit

Back up sensor

a. GPS Altitude
b. RPM Table

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12
Q

Which component is the MQ-5B Primary Airspeed sensor

A

ADU Air Data Unit

Back up sensor
Pitch table

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13
Q

Which component is the MQ – 5B Primary Heading sensor

A

INS internal navigation sensor

Back up sensor
FVU Flux valve unit

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14
Q

Which component is the MQ – 5B Primary Position sensor

A

INS/DGPS Internal Navigation Center/Differential Global Positioning System

Back up sensor

Back up DGPS differential global positioning system

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15
Q

Which component is the back up Heading sensor

A

FVU

Flux valve unit

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16
Q

Which component is the back up Position sensor

A

DGPS

Differential global position sensor

17
Q

Which component is the back up Attitude sensor

A

DMU

Dynamic measurement unit

18
Q

Which Component contains the auto pilot logic

A

MCPA modular central processing assembly

19
Q

How does the aircraft automatically make coordinated turns

A

ARI

Aileron Rudder Interconnect

20
Q

How far away Can the RVT to be from the aircraft and still receive video & telemetry

21
Q

Datalink system was designed to provide vacations between aircraft and ground antennas up to how many kilometers

22
Q

Which component is required for all parachute deployment

A

FTLU

Flight termination logic unit

23
Q

What are the basic components of the ERS

Emergency recovery system

A

Parachute, ordinance, FTLU, and MCPA

Flight termination logic unit

Modular central processor assembly

24
Q

How many and what type antennas are on the TGDT

A

3 - Directional, Omni, and GPS

25
What is the range of the GDT primary directional antenna
277 km
26
How many what type and what with cables connect a TGDT to an OSGCS
3-300 meter fiber optic cable single mode
27
Which hazard awareness statement as you to prove it bodily injured or death
Warning
28
Hazard awareness statement is used to prevent damage or destruction of equipment
Caution
29
What is the minimum allowable distance between open flames or lit cigarette and a fuel source
50 feet
30
How far away do personnel need to be if standing in line with a turning propeller
164 feet
31
What type of Eye protection is required within 164 feet of turning propellers
ANSI Z87.1
32
What location requires all personnel to wear safety shoes
Flightline